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Closed loop fiber optic rotation sensorAn improved optical gyroscope is provided, of the type that passes two light components in opposite directions through an optic fiber coil, and which adds a small variable frequency to one of the light components to cancel the phase shift due to rotation of the coil. The amount of coil rotation from an initial orientation, is accurately determined by combining the two light components, one of which has a slightly increased frequency, to develop beats that each represent a predetermined angle of rotation. The direction of rotation is obtained by combining the two light components on a photodetector, intermittently phase shifting a single light component by 90 deg and comparing the direction of change of photodetector output (+ or -) caused by the 90 deg shift, with the slope (+ or -) of the photodetector output at about the same time, when there is a 90 deg shift.
Document ID
19870013826
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Goss, Willis C.
(NASA Pasadena Office CA, United States)
Youmans, Bruce R.
(NASA Pasadena Office CA, United States)
Nerheim, Noble M.
(NASA Pasadena Office CA, United States)
Bartman, Randall K.
(Jet Propulsion Lab. California Inst. of Tech., Pasadena., United States)
Date Acquired
August 13, 2013
Publication Date
May 5, 1987
Subject Category
Optics
Report/Patent Number
Patent Number: NASA-CASE-NPO-16558-1-CU
Patent Application Number: US-PATENT-APPL-SN-779744
Patent Number: US-PATENT-4,662,751
Accession Number
87N23259
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-NPO-16558-1-CU|US-PATENT-4,662,751
Patent Application
US-PATENT-APPL-SN-779744
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